EP1516936A1 - Extremely fine shape memory alloy wire, composite material thereof and process for producing the same - Google Patents
Extremely fine shape memory alloy wire, composite material thereof and process for producing the same Download PDFInfo
- Publication number
- EP1516936A1 EP1516936A1 EP03736030A EP03736030A EP1516936A1 EP 1516936 A1 EP1516936 A1 EP 1516936A1 EP 03736030 A EP03736030 A EP 03736030A EP 03736030 A EP03736030 A EP 03736030A EP 1516936 A1 EP1516936 A1 EP 1516936A1
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- EP
- European Patent Office
- Prior art keywords
- alloy wire
- shape memory
- memory alloy
- resin
- composite material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/006—Resulting in heat recoverable alloys with a memory effect
Definitions
- the present invention relates to an extremely fine shape memory alloy wire, a composite material using the same, and a process for producing the same.
- products having a vibration-controlling function and exhibiting a retarded fatigue crack-developing rate can be obtained by embedding pre-strained shape memory alloy wires in a matrix of a carbon fiber reinforced plastic (CFRP), a glass fiber reinforced plastic (GFRP), aluminum (Al), or the like.
- CFRP carbon fiber reinforced plastic
- GFRP glass fiber reinforced plastic
- Al aluminum
- this technique can be applied to only composite materials which cure at 130°C. Namely, the technique cannot be applied to heat-resistant CFRP and GFRP to be molded at about 180°C, which are the most important in aviation and space industries.
- An object of the present invention is to provide a wire comprising a shape memory alloy in a martensitic phase which assumes an austenitic phase or a martensitic phase through phase transformation temperatures, which is capable of conjuncting with a resin at a high molding temperature of about 180°C, a composite material which comprises a resin comprising the wire, and a process for producing the same.
- an extremely fine wire having a diameter of 60 ⁇ m or less which is formed by a cold drawing work of a wire of the above shape memory alloy, is capable of easily conjuncting with a resin even at a high molding temperature of 180°C or higher. Based on this finding, they have accomplished the present invention.
- the following shape memory alloy wires, composite materials, and processes for producing the composite materials are provided.
- the shape memory alloy (hereinafter also simply referred to as "alloy") for use in the present invention is an alloy in a martensitic phase which assume an austenitic phase or a martensitic phase through phase transformation temperatures.
- Such an alloy includes a TiNi alloy.
- the Ni content thereof is from 49 to 52% by atom (at%).
- the shape memory alloy wire of the present invention is characterized in that the alloy wire is an extremely fine alloy wire having a diameter of 60 ⁇ m, which is formed by a cold drawing work of a wire of the above alloy, and the reverse transformation temperature thereof is at least 250°C.
- the diameter (thickness) is usually 60 ⁇ m or less, preferably 50 ⁇ m or less, and the lower limit is not particularly limited but is usually about 5 ⁇ m.
- the reverse transformation starting temperature (As) of the alloy wire is usually 130°C or higher, preferably 132°C or higher, and the upper limit is usually about 140°C.
- the reverse transformation termination temperature (Af) of the alloy wire is usually 250°C or higher, preferably 260°C or higher, and the upper limit is usually about 300°C.
- the alloy wire of the present invention is one which has been subjected to a cold drawing work.
- the cold drawing work means that an alloy wire is drawn at a temperature of 0 to 30°C, preferably 0 to 20°C.
- the cold drawing rate is at least 20%, preferably 30% or more, and more preferably 35% or more.
- the upper limit is usually about 50%.
- the As and Af of the alloy wire of the present invention can be controlled by the cold drawing rate, and the As and Af are also elevated according to increase of the cold drawing rate.
- the alloy wire which has been subjected to a cold drawing work according to the present invention retains a substantial amount of shrinking strain (pre-strain).
- the shrinking strain is 2% or more, preferably 2.5% or more, and more preferably 3.5% or more, and the upper limit is usually about 4%.
- the shrinking strain can be controlled by the drawing rate at the cold drawing of the alloy wire.
- the alloy wire of the present invention Since the alloy wire of the present invention has been subjected to a cold drawing work, the yield stress thereof is very large. Therefore, it affords a resin/wire composite material having enhanced strength and rigidity at a low temperature.
- the alloy wire in a martensitic phase of the present invention does not shrink substantially when heated at a temperature lower than the reverse transformation starting temperature (As) thereof but a phase change occurs when heated at a temperature of the reverse transformation termination temperature (Af) thereof or higher, so that the alloy wire is transformed to an alloy wire in an austenitic phase and shrinkage occurs.
- the alloy wire in an austenitic phase is again changed to a martensitic phase by cooling the wire to a low temperature.
- the As' and Af' in the alloy wire converted to the low-temperature martensitic phase is substantially the same as the As and Af in the alloy wire before the cold drawing work.
- the As' is about 20 to about 70°C and the Af' is about 30 to about 100°C.
- shrinkage occurs. The shrinkage in this case is nearly equal to that observed in a usual alloy wire in a martensitic phase.
- the temperature difference between the As and Af thereof is broad and the temperature difference is 130°C, preferably 150°C, and the upper limit is usually about 200°C.
- a temperature between the As temperature and Af temperature of the alloy wire is adopted as a molding temperature (a temperature for conjunction).
- Such a molding temperature is a temperature lower than the Af temperature of the alloy wire and the alloy wire is in an intermediate state between a martensitic phase and an austenitic phase, and hence the shrinking rate thereof is low. Therefore, a deformation ratio of the composite obtained by conjunction of the alloy wire with a resin is very small and thus does not particularly hinder usefulness of the composite.
- the shrinking strain is 3.5%, As is 133°C, and Af is 267°C (Fig. 1).
- the shrinking strain is 2.3%, As is 130°C, and Af is 210°C (Fig. 2).
- alloy wire/resin composite materials can be obtained by the use of the alloy wire of the present invention.
- the resin in this case includes a thermosetting resin and a thermoplastic resin.
- the thermosetting resin include an epoxy resin, a phenol resin, a polyimide resin, a vinyl ester resin, an unsaturated polyester resin, a polyurethane resin, a precured material of a thermosetting resin (thermosetting prepolymers), and the like.
- the thermoplastic resin include a polyolefin resin, a fluorine-containing resin, a polyamide resin, a thermoplastic polyimide resin, a polyester resin, a polycarbonate resin, and the like.
- the alloy wire for use in the composite material of the present invention can be used in combination with a conventionally known fibrous material, e.g., a glass fiber or a carbon fiber.
- the composite material of the present invention can be a thermosetting material (pre-impregnation material) comprising the alloy wire and a thermosetting resin or a precured material thereof (prepolymer).
- the composite material can be any of various shapes such as sheet, thread, columnar, rope, and block shapes.
- thermosetting composite material By heating the thermosetting composite material at a temperature lower than the Af of the alloy wire incorporated therein, usually a temperature of 185°C or lower to cure the resin, the material can be converted into a composite material comprising the alloy wire in the cured resin.
- the heating temperature is a temperature lower than the Af of the alloy wire, so that a large shrinkage of the alloy wire does not occur. Therefore, when the alloy wire of the present invention is used, it is actually not necessary to use both ends fixing apparatus which has been employed for retaining pre-strain of the wire in the cases of conventional alloy wires.
- the composite material comprising the alloy wire of the present invention in the cured resin can express a shrinking force through phase change from a martensitic phase to an austenitic phase by heating at least a part of the alloy wire to a high temperature of the Af thereof or higher.
- the alloy in an austenitic phase can be again converted into the alloy in a martensitic phase by further cooling the product to a low temperature.
- the product containing the alloy wire in a martensitic phase can be used in various applications utilizing characteristics of the alloy wire.
- the composite material of the present invention can be a material formed by embedding the alloy wire in a thermosetting resin and heating it at a temperature lower than the Af to cure the resin.
- the resin can be a liquid one or a powdery one.
- the resin can be one containing a fibrous material such as a glass fiber or a carbon fiber.
- the composite material of the present invention can be a material formed by thermally melting a thermoplastic resin which melts at a temperature lower than the Af of the alloy wire and arranging the alloy wire therein, followed by cooling and solidification.
- the As and Af thereof is not returned to normal ones unless the alloy is subjected to reverse transformation to an austenitic phase. Therefore, in the composite material, in order to obtain a shape-restoring power, it is necessary to heat the alloy wire in the composite material once to a temperature of the Af thereof or higher.
- heating of the alloy wire incorporated in the above composite material can be advantageously carried out by passing an electric current through part or all of the alloy wire for a short period and then shutting down the application of electric current.
- the period of the application of electric current is from 1 to 60 seconds, preferably from 1 to about 20 seconds.
- the alloy wire incorporated in the composite material By heating the alloy wire incorporated in the composite material to a temperature of the Af or higher and cooling it to a low temperature, the alloy wire is converted into a low temperature martensitic phase alloy wire, whose reverse transformation temperature returns to the normal one, and a shape-restoring power can be obtained by heating with a low current.
- CFRP carbon fiber reinforced epoxy resin
- Fig. 4 shows the results. From Fig. 4, it was revealed that the cold-drawn wire retained a shrinking strain of 2.5% even when thermally treated at 180°C for 2 hours. According to this shrinking strain of 2.5%, a shape-restoring stress of 250 MPa or more can be obtained.
- Figs. 5 and 6 shows experimental results on a crack-suppressing effect detected when the alloy wire in the composite material manufactured is heated by application of electric current.
- Fig. 5 shows a change of shrinking strain of the sample surface when an electric current is applied
- Fig. 6 shows a temperature change of the sample surface when an electric current is applied.
- a shape memory alloy wire advantageously applied to a resin having a high molding temperature of about 180°C, particularly a glass fiber reinforced resin and a carbon fiber reinforced resin.
- a shape memory alloy wire advantageously applied to a resin having a high molding temperature of about 180°C, particularly a glass fiber reinforced resin and a carbon fiber reinforced resin.
- the alloy wire of the present invention has a diameter which is so extremely fine as 60 ⁇ m or less, it can be handled in a similar manner to conventional carbon fibers and glass fibers. Therefore, according to the present invention, a prepreg composite material wherein the alloy wire is incorporated in a thermosetting resin can be obtained.
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- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Reinforced Plastic Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
- As:
- a reverse transformation starting temperature from a martensitic phase to an austenitic phase formed when an alloy wire is heated in the direction of the arrow a.
- Af:
- a reverse transformation termination temperature from a martensitic phase to an austenitic phase formed when an alloy wire is heated in the direction of the arrow a.
- Ms:
- a reverse transformation starting temperature from an austenitic phase to a martensitic phase formed when an alloy wire is cooled in the direction of the arrow a.
- Mf:
- a reverse transformation termination temperature from an austenitic phase to a martensitic phase formed when an alloy wire is cooled in the direction of the arrow a.
- As' :
- a reverse transformation starting temperature from a martensitic phase to an austenitic phase formed when an alloy wire is heated in the direction of the arrow b.
- Af':
- a reverse transformation termination temperature from a martensitic phase to an austenitic phase formed when an alloy wire is heated in the direction of the arrow b.
Claims (15)
- A shape memory alloy wire subjected to a cold drawing work, which comprises a shape memory alloy in a martensitic phase which assumes an austenitic phase or a martensitic phase through phase transformation temperatures, has a diameter of 60 µm or less, and has a reverse transformation termination temperature of at least 250°C.
- The shape memory alloy wire according to claim 1, which has a cold drawing rate of at least 20%.
- The shape memory alloy wire according to claim 1 or 2, wherein the shape memory alloy is a Ti-Ni alloy.
- A composite material which comprises a fibrous material and a resin, wherein the fibrous material comprises the shape memory alloy wire according to any one of claims 1 to 3.
- A composite material which comprises a fibrous material and a resin, wherein the fibrous material comprises the shape memory alloy wire according to any one of claims 1 to 3 and at least one fiber selected from a glass fiber and a carbon fiber.
- The composite material according to claim 4 or 5, wherein the resin comprises a thermosetting resin or a thermoplastic resin.
- The composite material according to claim 4 or 5, wherein the resin comprises a precured material of a thermosetting resin.
- The composite material according to claim 4 or 5, wherein the resin comprises a thermoset product of a thermosetting resin.
- The composite material according to any one of claims 4 to 8, wherein the thermosetting resin comprises an epoxy resin.
- A composite material which comprises a cured resin comprising the shape memory alloy wire according to any one of claims 1 to 3, wherein the shape memory alloy wire is heated to a temperature of a reverse transformation termination temperature thereof or higher to generate a contractive force.
- The composite material according to claim 10, which comprises at least one fiber selected from a glass fiber and a carbon fiber together with the shape memory alloy wire.
- The composite material according to claim 10 or 11, wherein said heating of the shape memory alloy wire is carried out by application of electric current to the wire.
- A process for producing a composite material, which comprises heat-curing a thermosetting resin or a precured material thereof comprising the shape memory alloy wire according to any one of claims 1 to 3 at a temperature which is a reverse transformation starting temperature of the shape memory alloy wire or higher and is lower than the reverse transformation termination temperature; and then heating at least a part of the shape memory alloy wire to a temperature of its reverse transformation final temperature or higher.
- The process according to claim 13, wherein the thermosetting resin or the precured material thereof comprises at least one fiber selected from a glass fiber and a carbon fiber.
- The process according to claim 13 or 14, wherein said heating of the shape memory alloy wire is carried out by application of electric current to the wire.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2002162287 | 2002-06-04 | ||
| JP2002162287 | 2002-06-04 | ||
| PCT/JP2003/007084 WO2003102256A1 (en) | 2002-06-04 | 2003-06-04 | Extremely fine shape memory alloy wire, composite material thereof and process for producing the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1516936A1 true EP1516936A1 (en) | 2005-03-23 |
| EP1516936A4 EP1516936A4 (en) | 2005-08-31 |
Family
ID=29706602
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03736030A Withdrawn EP1516936A4 (en) | 2002-06-04 | 2003-06-04 | EXTREMELY NARROW YARN OF SHAPE MEMORY ALLOY, COMPOSITE MATERIAL FOR THE PRODUCTION THEREOF AND PROCESS FOR PRODUCING THE SAME |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP1516936A4 (en) |
| JP (1) | JP4168151B2 (en) |
| AU (1) | AU2003242038A1 (en) |
| WO (1) | WO2003102256A1 (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2441589A (en) * | 2006-09-05 | 2008-03-12 | Anthony Walter Anson | Heat treatment method for composite textiles |
| WO2010127646A2 (en) | 2009-05-04 | 2010-11-11 | Institute Of Physics As Cr, V. V. I. | A method of heat treatment and/or inspection of functional mechanical properties, particularly transformation strain and/or strength, of shape memory alloy filaments and apparatus for the application of this method |
| DE102009038204A1 (en) | 2009-08-20 | 2011-04-21 | Siemens Aktiengesellschaft | Solar-powered actuator e.g. electrical actuator, for driving e.g. window blind, of industrial building installation, has wire whose end is coupled to installation, so that installation or installation part is moved during elongation of wire |
| US9314885B2 (en) | 2012-05-11 | 2016-04-19 | Empire Technology Development Llc | Shape memory alloy composite flexible substrates |
| CN107936559A (en) * | 2017-11-30 | 2018-04-20 | 万丰航空工业有限公司 | The three-dimensional carbon fiber of a kind of selfreparing/memorial alloy aircraft shell and preparation method thereof |
| US12385473B1 (en) | 2024-10-30 | 2025-08-12 | Blue Origin Manufacturing, LLC | Semi-passive linear actuator |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7431981B2 (en) * | 2002-11-04 | 2008-10-07 | The Boeing Company | Polymer composite structure reinforced with shape memory alloy and method of manufacturing same |
| CN112935009B (en) * | 2021-02-27 | 2022-06-17 | 苏州英忆新材料有限公司 | Production method of orthodontic wire capable of automatically shaping oral cavity |
| CN112872087B (en) * | 2021-02-27 | 2022-06-17 | 苏州英忆新材料有限公司 | Production method of memory alloy wire capable of being automatically shaped |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06212018A (en) * | 1993-01-14 | 1994-08-02 | Yasubumi Furuya | Polymer-based material having composite functions |
| DE4307593C1 (en) * | 1993-03-10 | 1994-08-04 | Fraunhofer Ges Forschung | Filament structure of shape memory alloy wires |
| JPH07133743A (en) * | 1993-11-09 | 1995-05-23 | Mitsubishi Heavy Ind Ltd | Shape memory alloy fiber reinforced aluminum |
| JPH07197221A (en) * | 1993-12-28 | 1995-08-01 | Furukawa Electric Co Ltd:The | Method for manufacturing Ni-Ti-Pd type shape memory alloy element |
| JPH0813068A (en) * | 1994-07-01 | 1996-01-16 | Unitika Ltd | Ti-ni based fine metallic wire |
| EP0709482B1 (en) * | 1994-10-28 | 1999-07-28 | Kazuhiro Otsuka | Method of manufacturing high-temperature shape memory alloys |
| US5614305A (en) * | 1995-02-08 | 1997-03-25 | Virginia Tech Intellectual Properties, Inc. | Impact and perforation resistant composite structures |
| JP3474342B2 (en) * | 1995-12-26 | 2003-12-08 | 科学技術振興事業団 | Composite material with fracture progress prevention function and fracture progress prevention system |
| JPH09317821A (en) * | 1996-05-27 | 1997-12-12 | Mitsubishi Heavy Ind Ltd | Functional structural material |
| JPH09208739A (en) * | 1997-01-13 | 1997-08-12 | Tokin Corp | Sheet-shaped composite material |
| JP4113941B2 (en) * | 2001-05-29 | 2008-07-09 | 独立行政法人産業技術総合研究所 | Functional composite material using shape memory alloy and method for producing the same |
-
2003
- 2003-06-04 EP EP03736030A patent/EP1516936A4/en not_active Withdrawn
- 2003-06-04 JP JP2004510490A patent/JP4168151B2/en not_active Expired - Lifetime
- 2003-06-04 WO PCT/JP2003/007084 patent/WO2003102256A1/en not_active Ceased
- 2003-06-04 AU AU2003242038A patent/AU2003242038A1/en not_active Abandoned
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2441589A (en) * | 2006-09-05 | 2008-03-12 | Anthony Walter Anson | Heat treatment method for composite textiles |
| WO2010127646A2 (en) | 2009-05-04 | 2010-11-11 | Institute Of Physics As Cr, V. V. I. | A method of heat treatment and/or inspection of functional mechanical properties, particularly transformation strain and/or strength, of shape memory alloy filaments and apparatus for the application of this method |
| DE102009038204A1 (en) | 2009-08-20 | 2011-04-21 | Siemens Aktiengesellschaft | Solar-powered actuator e.g. electrical actuator, for driving e.g. window blind, of industrial building installation, has wire whose end is coupled to installation, so that installation or installation part is moved during elongation of wire |
| US9314885B2 (en) | 2012-05-11 | 2016-04-19 | Empire Technology Development Llc | Shape memory alloy composite flexible substrates |
| CN107936559A (en) * | 2017-11-30 | 2018-04-20 | 万丰航空工业有限公司 | The three-dimensional carbon fiber of a kind of selfreparing/memorial alloy aircraft shell and preparation method thereof |
| CN107936559B (en) * | 2017-11-30 | 2020-03-17 | 万丰飞机工业有限公司 | Self-repairing three-dimensional carbon fiber/memory alloy aircraft shell and preparation method thereof |
| US12385473B1 (en) | 2024-10-30 | 2025-08-12 | Blue Origin Manufacturing, LLC | Semi-passive linear actuator |
Also Published As
| Publication number | Publication date |
|---|---|
| JP4168151B2 (en) | 2008-10-22 |
| EP1516936A4 (en) | 2005-08-31 |
| JPWO2003102256A1 (en) | 2006-03-16 |
| WO2003102256A1 (en) | 2003-12-11 |
| AU2003242038A1 (en) | 2003-12-19 |
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